Page 4.8 Chapter 4 Airworthiness Limitations MAY 2015
14 CFR part 27.695(a)(1), Power boost and power-operated control system.
(see Note 7)
Special Condition:
No. 27-035-SC Robinson Model R66 Helicopter, Sec. 27.1309, Installation of
HeliSAS Autopilot and Stabilization Augmentation System (AP/SAS).
14 CFR Part 36, dated December 1, 1969, as amended by Amendment 36-1
through Amendment 36-28.
Compliance with the ditching requirements of § 27.801 was not demonstrated.
Compliance with the ice protection requirements of § 27.1419 was not
demonstrated.
The R66 is approved for day and night VFR operations only.
TC Application Date: September 06, 2006.
TC Issue Date: October 25, 2010.
Production Basis Production Certificate No. 424WE dated October 25, 2010.
Equipment The basic required equipment as prescribed in the applicable airworthiness
regulations (see Certification Basis) must be installed in the aircraft for
certification. In addition, the following FAA-approved Rotorcraft Flight
Manual is required:
R66 Pilot’s Operating Handbook and FAA Approved Rotorcraft Flight
Manual (RTR 661), dated October 25, 2010, or later approved revision.
GENERAL NOTES
NOTE 1. A current weight and balance report, including a list of equipment included in the certificated
empty weight, and loading instructions when necessary, must be provided for each aircraft at the
time of original airworthiness certification and at all times thereafter, except in the case of
operators having an approved weight control system.
NOTE 2. The following placard must be installed in clear view of the pilot:
“THIS ROTORCRAFT APPROVED FOR DAY AND NIGHT VFR OPERATIONS”
For additional placards, see the Rotorcraft Flight Manual. All placards required in the Rotorcraft
Flight Manual must be installed in the appropriate locations.
NOTE 3. Information essential to the proper maintenance of the helicopter, including retirement time of
critical components, is contained in the Robinson R66 Maintenance Manual and Instructions for
Continued Airworthiness (RTR 660). Retirement times are listed in the “AIRWORTHINESS
LIMITATIONS” section.
NOTE 4. Deleted as of March 10, 2015.
NOTE 5. Any cockpit instruments installed by a 3
rd
party must be marked with limit markings and range
markings in accordance with Robinson’s marking scheme.
NOTE 6. Deleted as of March 10, 2015.
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